US3267946A - Flow control apparatus - Google Patents

Description

1966 R. B. ADAMS ET AL 3261946 FLOW CONTROL APPARATUS Filed April 12, 1963 5 Sheets-Sheet 1.

INVENTORS ROBERT E. ADAMS COL [MAN 8. MOORE AT T ORA/E V 23, 1966 R. B. ADAMS ET AL 3,267,946

FLOW CONTROL APPARATUS Filed April 12, 1963 5 Sheets-Sheet 8 INVENTORS ROBERT E. ADAMS COL EMA/V 8. MOORE ATTORNEY Aug. 23, 1966 R. B. ADAMS ETAL 3,267,946 FLOW CONTROL APPARATUS Filed April 12, 1963 5 Sheets-Sheet 5 I N VEN TORS ROBERT E. ADAMS COL MA/V 8.MOORE 7/ gr m? ATTORNEY United States Patent 3,267,946 FLGW CGNTROL APPARATUS Robert B. Adams, Abington, and Coleman B. Moore,

Uwehland, Pa, assignors to Moore Products Co., Philadelphia, Pa, a corporation of Pennsylvania Filed Apr. 12, 1963, Ser. No. 272,663

11 Claims. (Cl. 13781.5)

This invention relates to fluid flow control apparatus.

It has heretofore been proposed to control the direction of flow of a jet of fluid in accordance with a signal applied to control ports positioned in a jet interaction chamher and to separate the jet into streams having different quantities therein.

It is the principal object of the present invention to provide flow control apparatus in which the directional positioning of a fluid jet is utilized to determine the impedance to fluid flow in the apparatus.

It is a further object of the present invention to provide flow control apparatus in which a vortex chamber has a fluid jet directed thereinto, the control of the direction of the fluid jet determining the impedance action of the chamber.

It is a further object of the present invention to provide flow control apparatus having a fluid jet communicating with a chamber at a selected direction, the control of the direction determining the proportioning action of the apparatus.

It is a further object of the invention to provide fluid flow control apparatus in which accurate control of proportioning can be obtained over a wide range of operating conditions.

It is a further object of the present invention to provide fluid flow control apparatus in which a jet is directionally controlled to determine the flow and in which no mechanical moving parts are employed at or along the controlling jet.

It is a further object of the present invention to provide apparatus of the character aforesaid capable of control by a single signal, and in which the structure is readily reversible as to the effect of the signal.

It is a further object of the present invention to pro vide fluid flow control apparatus in which a jet is directionally controlled to determine the flow and in which no mechanical moving parts are employed at or along the controlled jet, the range being enhanced by the use of auxiliary structure.

Other objects and advantageous features of the invention will be apparent from the description and claims.

The nature and characteristic features of the invention will be more readily understood from the following description, taken in connection with the accompanying drawings forming part thereof, in which:

FIGURE 1 is a top plan view of one preferred form of fluid flow control apparatus in accordance with the invention, with a single control port, part of the cover plate being broken away:

FIG. 2 is a vertical sectional view taken approximately on the line 2- 2 of FIG. 1 and showing one form of vortex chamber;

FIG. 3 is a vertical sectional view taken approximately on theline 33 of FIG. 1;

FIG. 4 is a fragmentary vertical sectional view similar to FIG. 2, showing another form of vortex chamber;

FIG. 5 is a top plan view of another preferred form of fluid flow control apparatus in accordance with the invention, with a pair of control ports, part of the cover plate being broken away;

\FIG. 6 is a vertical sectional view taken approximately on the line 6-6 of FIG. 5;

FIG. 7 is a vertical sectional view taken approximately on the line 77 of FIG. 5;

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FIG. 8 is a top plan view of another preferred form of fluid flow control apparatus in accordance with the invention part of the cover plate being broken away;

FIG. 9 is a vertical sectional view taken approximately on the line 99 of FIG. 8;

FIG. 10 is a horizontal sectional view of another preferred form of fluid flow control apparatus in accordance with the invention with reversibility of the assembly for control; and

FIG. 11 is a view similar to FIG. 10 showing another preferred form of fluid flow control apparatus with reversibility of the assembly for control.

It should, of course, be understood that the description and drawings herein are illustrative merely, and that various modifications and changes can be made in the structure disclosed without departing from the spirit of the invention.

Like numerals refer to like parts throughout the several views.

Fluid flow control devices have been proposed in which the flow is controlled by pure fluid interaction of a jet discharging into an interaction chamber which chamber has opposite side Walls symmetrical with respect to the longitudinal axis of the jet. In such devices regions on both sides of the jet delineated by the side walls of the interaction chamber and the jet stream had one control connection or opposite control connections contiguous to the entrance location of the jet for input or discharge as determined by the relation of pressure conditions in the chamber to the ambient pressure.

In fluid flow devices, also, vortex chambers of various shapes and the flow of fluid therein have been known.

The present invention utilizes a jet interaction chamber with a vortex chamber to provide a variable impedance to fluid flow.

Referring now more particularly to FIGS. 1, 2 and 3 of the drawings, acover plate 15 is shown which can be of generally rectangular or other shape as desired, with anupper face 16 and alower face 17. Theplate 15 can be made of any desired material, such as metal, synthetic resinous plastic or the like, which is not subject to corrosion by the fluid or fluids in contact therewith.

Anintermediate plate 18 is provided which can also be of any suitable material with anupper face 19 and alower face 20, and with the interior thereof shaped as hereinafter described.

Abottom closure plate 21 is provided, of any desired material, having anupper face 22 and alower face 23.

Theplates 15, 18 and 21 are secured together in any desired manner with thefaces 17 and 19 and the faces 20 and 22 in fluid tight engagement. For this purpose,bolts 24 havingwashers 25 under their heads. can be provided in threaded engagement inopenings 26 in thebottom plate 21.

Theplate 18 has afluid inlet passageway 23 provided therein with which afluid supply connection 30 is in communication through theplate 21. Thefluid supply connection 30 can have the fluid Whose flow is to be controlled supplied thereto, and the fluid can be liquid or gaseous, as desired.

Theplate 18 has anozzle 32 with which thepassageway 28 is in communication. Thenozzle 32 communicates with aninteraction chamber 33 having opposite divergingwall portions 34 and 34a, asymmetrical to impart a bias to one wall portion. For example,portion 34 contiguous to thenozzle 32 may be set back. Theinteraction chamber 33 also has continuousreturn wall portions 35 and 35a. Extending to thechamber 33, immediately beyond thenozzle 32, acontrol fluid connection 36 is provided. Thefluid connection 36 is connected to a source of fluid. For this purpose afluid connection 37 can extend to thefluid supply connection 30 with avalve 38 interposed 3 therein and can also, if desired, be connected to an independent source of fluid, such as by a fluid connection 39 with avalve 40 interposed therein.

Theplate 18, beyond the termini of thewall portions 35 and 35:: has avortex chamber 45 therein, shown in FIGS. 1, 2 and 3, as cylindrical, and bounded by thelower face 17 of the plate and theupper face 22 of theplate 21. Thevortex chamber 45 has a central discharge opening 46 from which afluid delivery pipe 47 extends.

Athroat 48 is provided between theinteraction chamber 33 and thevortex chamber 45. The longitudinal axis of the jet established by thenozzle 32 and thewall portions 35 and 35a is disposed so that the direction of delivery of the jet into thevortex chamber 45 can be varied as desired over a wide range of positions between predetermined limits of radial and peripheral delivery. A jet travelling along thewall portions 34 and 35 and entering thevortex chamber 45 will move substantially radially in thechamber 45 toward thedischarge opening 46. A jet travelling along thewall portions 34a and 35a will enter thevortex chamber 45 substantially tangentially and travel in a spiral path to thedischarge opening 46. Intermediate the two extreme or limit positions of the jet just referred to, other positions of the jet will be available.

Referring now more particularly to FIG. 4 of the drawings another form ofvortex chamber 145 is shown in which thechamber 145 has a curvedlower boundary wall 50 of curved or funnel shape provided in thelower plate 21 with an upperflat boundary wall 17 provided by theupper plate 15. A central discharge opening 146 offset from the plane of the inlet to thechamber 145 is provided for discharge of the fluid for delivery.

Referring now more particularly to FIGS. 5, 6 and 7 of the drawings an embodiment of the invention is shown in which a pair of central ports are employed in the jet interaction chamber.

Thecover plate 215, of generally rectangular shape, has anupper face 216 and alower face 217, and is made of any desired material, as before.

Theintermediate plate 218, also of any desired material, has anupper face 219 for engagement with thelower face 217 and has alower face 220.

Abottom plate 221 is also provided, having anupper face 222 for engagement with thelower face 220 and alower face 223.

Theplates 215, 218 and 221 are secured together, as before, bybolts 224 havingwashers 225 under their heads, thebolts 224 engaging in threadedopenings 226 in thebottom plate 221.

Theplate 218 has afluid inlet passageway 228 provided therein with which afluid supply connection 230 is in communication.

Theplate 218 has anozzle 232 with which thepassageway 228 is in communication. Thenozzle 232 communicates with aninteraction chamber 233 having opposite symmetrical divergingwall portions 234 and 23411 and continuousreturn wall portions 235 and 235a. In thechamber 233, immediately beyond thenozzle 232, oppositecontrol fluid connections 236 are provided. Thefluid connections 236 are connected bypipes 52 and 53 toports 54 and 55 in acontrol valve housing 56. Thehousing 56 can have a manually or otherwiseoperable valve plug 57 therein for controlling theports 54 and 55 and the flow of fluid through thepipes 52 and 53. Theinlet 58 to thehousing 56 can be connected to a source of fluid, as desired.

Theplate 218, beyond the termini of thewall portions 235 and 235a has avortex chamber 245 therein, shown as cylindrical, bounded by thelower face 217 of theplate 216 and theupper face 222 of theplate 221. Thevortex chamber 245 has a central discharge opening 246 from which -afluid delivery pipe 247 extends.

Athroat 248 is provided between the interaction chamber 2'33 and thevortex chamber 245. The longitudinal axis of the jet established by thenozzle 232 and thewall portions 234 and 234a is disposed so that a jet travelling along the wall portions 23'4a and 235a will move substantially radially in thevortex chamber 245 toward the disc-barge opening 246 and so that a jet travelling along thewall portions 234 and 235 will enter thevortex chamber 245 substantially tangentially and for travel in a spiral path to thedischarge opening 246. Intermediate the two limit or extreme positions of the jet just referred to, other positions of the jet will be available.

The length of theinteraction chambers 33 and 233 can be selected as desired, but are preferably such that the ratio of the chamber length to the nozzle width is in the range from about seven to one to about five to one.

Referring now more particularly to FIGS. 8 and 9, the structure there shown in generally similar to that shown in FIGS. 1 and 2, with afluid inlet passageway 28,nozzle 32,interaction chamber 33, divergingwall portions 34 and 34a, returnwall portions 35 and 35a, controlfluid connection 36 andthroat 48.

Thevortex chamber 345 is greater in height than the height of thethroat 48 with upper and lower bounding faces 317 and 322. Acentral discharge opening 346 has aventuri 60 therebelow with afluid connection 61, a convergingventuri approach section 62, aventuri throat 63, and a divergingrecovery section 64 connected to adischarge pipe 347.

Referring now more particularly to FIG. 10, the const-ruction there illustrated is made of a plurality of castings or preformed sections including asupply housing section 65 with afluid inlet passageway 428, to which asupply connection 30 is connected, anozzle section 66 with anozzle 432, aninteraction chamber section 67 with aninteraction chamber 433 therein, and avortex chamber section 68 with avortex chamber 445 therein.

Thesupply housing section 65 andinteraction chamber section 67 haveflanges 69 and 70 for clamping of anozzle section 66 of selected size therebetween dependent upon the nozzle characteristics desired. Theflanges 69 and 7t} and the selectednozzle section 66 can be held in assembled relation bybolts 71.

Thevortex chamber section 68 andinteraction chamber section 67 are also held in assembled relation and in selected orientation bybolts 72. A singlecontrol fluid connection 436 can be employed, dependent upon the orientation of theinteraction chamber section 67 with respect to thevortex chamber section 68, to direct the jet from thenozzle section 66 either toward the periphery of thevortex chamber 445 or toward thedischarge opening 446 for a particular control fluid condition. In this manner it is possible for an increase in the control fluid supplied through thefluid connection 436 to cause an increase in the flow through the delivery connection for one arrangement or for an increase in the control fluid supplied to cause a decrease in the flow through the delivery connect-ion for the opposite arrangement.

FIGURE 11 shows an alternate vortex arrangement for controlling the discharge of fluid. As shown here, this construction comprises three main body portions; aninlet section 565 having anozzle 532, afluid interaction section 567 having therein afluid interaction chamber 533, two fluid passageways 74 and separated by adivider 73 are contiguous withchamber 533 and acontrol fluid passageway 536 communicates withinteraction chamber 533 along one of its side walls 534a adjacent to the point of entry of the fluid jet at 532. Theopposite side wall 534 is offset slightly from the enteringjet 532. A vortex section comprising acylindrical vortex chamber 545 having aco-axial outlet 546 in one end is attached to thefluid interaction section 567 so that thepassageways 74 and 75 continue and enter the vortex chamber, one being directed radially and the other tangentially with respect to thevortex chamber 545. The means of attachinginteraction chamber 567 to the vortex chamber 568 is symmetrical with respect to passageways '74 and 75 so that the assembly may be assembled in reverse relationship to that illustrated, thereby reversing the effect of the control fluid at 536 on the discharge of fluid through thedelivery connection 546. In this manner it is possible for an increase in the control fluid supplied through thefluid connection 536 to cause a decrease in flow through delivery connection for one arrangement, as

. shown, or for an increase in the control fluid supplied to cause an increase in the flow through the delivery connection for the opposite arrangement.

The mode of operation will now be pointed out reference being had first to FIGS. 1, 2 and 3.

Assume that fluid is supplied through thefluid supply connection 30, through thefluid inlet passageway 28 and thenozzle 32 into theinteraction chamber 33.

If thefluid connection 36 is open and capable of supplying fluid, such fluid will create a higher pressure condition along thewall portion 34a than along thewall portion 34 so that the jet is influenced to move to the wall portion '34 and will continue along thewall 35 and enter thevortex chamber 45 substantially radially. If thefluid connection 36 is closed, then the jet will favor flowing along the wall portion 34:: because of the set back of thewall portion 34 from thenozzle 32 and the absence of set back of thewall portion 34a, and will continue along thewall 35a and will enter thevortex chamber 45 substantially tangentially.

Assume further that the fluid pressure conditions in thechamber 33 as determined by the pressure conditions 'at thecontrol fluid connection 36 are such that the flow is radial. This direct radial flow is the condition of minimum impedance and accordingly of maximum flo w.

-If now the pressure conditions at thecontrol fluid connection 36 are changed, such as by partial reduction of fluid supplied therethough, as controlled by thevalve 38 with thevalve 41 closed, or by thevalve 41 with thevalve 38 closed, the impedance will be increased as the delivery through thethroat 48 is shifted to a lesser or greater extent from the initial radial path referred to.

The maximum impedance will be that in which the jet from thenozzle 32 is directed so as to enter thevortex chamber 45 peripherally or tangentially, with the maximum vortex action in thevortex chamber 45 providing a maximum impedance.

The impedance for intermediate angular positions of entry into thevortex chamber 45 of the jet from theinteraction chamber 33 will vary between the limits for the entry positions of the jet and in a manner wihch permits of proportional control of the flow to thedischarge opening 46 anddelivery pipe 47.

-Referring now to FIGS. 5, 6 and 7, the operation of the structure there shown is similar to that previously described except that the jet positioning will be subject to the opposite signals available at thefluid connections 235, as determined by the positioning of thevalve 57 with respect to theports 54 and 55.

Referr ng now to FIGS. 8 and 9, the operation of the structure there shown is also similar to that previously described except that the interposition of the venturi between thevortex chamber 34 and thedischarge pipe 346 gives an increase in the range of proportioning. This is based on the flow characteristics of a venturi in which fluid flowing in a swirling path at the entrance is impeded more than that having a straight line flow pattern at the entrance. 1

Referring now to FIG. 10, the operation of that structure is similar to those previously discussed with reversibility of the effect of the control pressure if desired.

Referring now to FIG. 11 a radial fluid path at 74 is provided at the entrance to thevortex chamber 545 and a tangential fluid path is provided at 75. These passageways at 74 and 75 receive fluid from thenozzle 532 in jet form and under the control of the fluid supplied in thefluid connection 536.

With suflicient fluid supplied through thefluid connection 536 the entire jet will be directed through thepassageway 75 giving the maximum restrictive action in thevortex chamber 545.

With thefluid connection 536 closed the entire jet will be directed through the passageway 74, giving the minimum restrictive action in thevortex chamber 545.

At intermediate fluid supply conditions in thefluid connection 536, the jet will be split by thedivider 73 so that different proportions are directed through passageways 74 and '75 giving intermediate restrictive actions in thevortex chamber 545.

We claim:

I. Fluid flow control apparatus comprising a vortex chamber whose section is substantially a circle in one plane,

said vortex chamber having an outlet axially disposed with respect to said chamber section,

a fluid inlet portion in the peripheral wall of said chamber,

means exteriorly of said chamber for supplying a fluid jet through said inlet portion,

said means having members for varying the direction of said jet at the point where it enters said chamber in a range between delivery radially toward said vortex chamber outlet and tangentially in said vortex chamber for discharge.

2. Fluid flow control apparatus as defined inclaim 1 in which said means comprises a fluid interaction chamher with a nozzle for initially directing the jet thereinto, said interaction chamber has opposite side Walls, and said direction varying members include a fluid connection to at least one of said side Walls controlling the positioning of the jet.

3. Fluid flow control apparatus as defined inclaim 1 in which said fluid interaction device has a divider therein for forming said throat portion and for separating the fluid from said nozzle into two streams.

4. Fluid flow control apparatus as defined inclaim 1 in which said fluid interaction device is reversibly mounted with respect to said vortex chamber about the longitudinal axis of said inlet nozzle.

5. Fluid flow control apparatus as defined inclaim 1 in which a separable nozzle is provided.

6. Fluid flow control apparatus comprising a vortex chamber having a central discharge opening, said vortex chamber at the periphery thereof having an inlet portion With a part directing fluid radially interiorly of said chamber and a part directing fluid tangentially interiorly of said chamber, a source of fluid, and means exteriorly disposed with respect to said vortex chamber for varying the distribution of fluid from said source between said parts of said inlet portion comprising a fluid interaction chamber outside said vortex chamber into which the fluid from said source is delivered, said fluid interaction chamber having a control fluid connection connected thereto, said fluid interaction chamber being asymmetrical and having a single control port therein.

7. Fluid flow control apparatus comprising a vortex chamber having an inlet portion at the side thereof and a central discharge opening, and members for delivering a fluid jet into said vortex chamber at said inlet portion, said last members including a member for varying the direction of delivery of said jet into said vortex chamber in a range between delivery radially toward said discharge opening and peripherally in said vortex chamber, said vortex chamber having the discharge opening of converging shape merging with the vortex chamber.

8. Fluid flow control apparatus comprising a vortex chamber having an inlet portion at the side thereof and a central discharge opening, and members for delivering a fluid jet into said vortex chamber at said inlet portion, said last members including a member for varying the direction of delivery of said jet into said vortex chamber in a range between delivery radially toward said discharge opening and peripherally in said vortex chamber, said vortex chamber at the discharge opening having a device connected thereto with greater resistance to swirling flow than to straight flow.

9. Fluid flow control apparatus comprising a vortex chamber having an inlet portion at the side thereof and a central discharge opening, and members for delivering a fluid jet into said vortex chamber at said inlet portion, said last members including a member for varying the direction of delivery of said jet into said vortex chamber in a range between delivery radially toward said discharge opening and peripherally in said vortex chamber, said vortex chamber at the discharge opening having a venturi device connected thereto.

10. Fluid flow control apparatus comprising a vortex chamber having an inlet portion at the side thereof and a central discharge opening, and members for delivering fluid into said vortex chamber at said inlet portion, said last members including a fluid interaction device having an inlet nozzle, side walls extending beyond said nozzle and a fluid control connection to at least one of said side walls, said vortex chamber at the discharge opening having a device connected thereto with greater resistance to swirling flow than to straight flow.

11. Fluid flow control apparatus comprising a vortex chamber having an inlet portion at the side thereof and a central discharge opening, and members for delivering fluid into said vortex chamber at said inlet portion, said last members including a fluid interaction device having an inlet nozzle, side walls extending beyond said nozzle and a fluid control connection .to at least one of said side walls, said vortex chamber at the discharge opening having a venturi device connected thereto.

References Cited by the Examiner UNITED STATES PATENTS OTHER REFERENCES Fluid let Control Devices, A.S.M.E. T] 935, S95, 1962 C. 2 p. 8.

M. CARY NELSON, Primary Examiner.

LAVERNE D. GEIGER, Examiner.

S. SCOTT, Assistant Examiner.

Claims (1)

1. FLUID FLOW CONTROL APPARATUS COMPRISING A VORTEX CHAMBER WHOSE SECTION IS SUBSTANTIALLY A CIRCLE IN ONE PLANE, SAID VORTEX CHAMBER HAVING AN OUTLET AXIALLY DISPOSED WITH RESPECT TO SAID CHAMBER SECTION, A FLUID INLET PORTION IN THE PERIPHERAL WALL OF SAID CHAMBER, MEANS EXTERIORLY OF SAID CHAMBER FOR SUPPLYING A FLUID JET THROUGH SAID INLET PORTION, SAID MEANS HAVING MEMBERS FOR VARYING THE DIRECTION OF SAID JET AT THE POINT WHERE IT ENTERS SAID CHAMBER IN A RANGE BETWEEN DELIVERY RADIALLY TOWARD SAID VORTEX CHAMBER OUTLET AND TANGENTIALLY IN SAID VORTEX CHAMBER FOR DISCHARGE.

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